STC SR00368BO

Number SR00368BO

FAA Form 8110-2 (03/21) SUPERSEDES PREVIOUS EDITION Page 1 of 3 This certificate issued to:

Outerlink Corporation 150 Baker Avenue Ext., Suite 302 Concord, MA 01742-2199 Part 27 of the Federal Aviation Regulations.

Original Product - Type Certificate Number: H88EU Make: Airbus Helicopters Deutschland GmbH Model: EC135 P1, P2, P2+, P3, T1, T2, T2+, and T3 Description of Type Design Change:

Helicopters modified with an Installation of an Outerlink SATCOM Communications and Flight Data Monitoring System KIT 135-SAT-100 in accordance with Outerlink Corporation's Master Drawing Lists (MDL), Document number MDL135-SAT-100, revision IR, dated February 18, 2016 or later FAA approved revisions of these documents. Operation must be in accordance with Outerlink Corporation’s Rotorcraft Flight Manual Supplement (RFMS) Document Number FMS135SAT001, revision B, dated January 21, 2016 which was FAA approved on May 16, 2016, or later FAA approved revisions. Maintenance must be in accordance with Instructions for Continued Airworthiness (ICA), document number ICA135SAT001, revision: C, April 22, 2016, or later FAA accepted revision. (continued on Page 3 of 3)

Date of Application: August 24, 2015 Date reissued: March 29, 2023

Date of Issuance: May 26, 2016 Date amended:

Signature Nicholas Faust

Manager, Boston Aircraft Certification Office Title

Number SR00368BO

FAA Form 8110-2 (03/21) SUPERSEDES PREVIOUS EDITION Page 2 of 3

To (Name and address of transferee) Name:

Address (Number and Street, City, State, and ZIP Code):

From (Name and address of grantor) Name:

Address (Number and Street, City, State, and ZIP Code):

(Continuation Sheet) Number SR00368BO

FAA Form 8110-2 (03/21) SUPERSEDES PREVIOUS EDITION Page 3 of 3 May 26, 2016 Limitations and Conditions:

1. The RFMS must be carried in the aircraft during all flights.

2. The ICA must be made available to the operator at the time of installation.

3. This system does not meet the operational rule requirement of a voice or flight data recorder system.

4. Compatibility of this design with previously approved modifications must be determined by the installer.

Certification Basis:

Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48, the certification basis for the Airbus Helicopters Deutschland GmbH models EC135 P1, P2, P2+, P3, T1, T2, T2+ and T3 is as follows:

a. The type certification basis for Airbus Helicopters Deutschland GmbH models EC135 P1, P2, P2+, P3, T1, T2, T2+ and T3 aircraft is shown on TCDS H88EU for parts not changed or not affected by the change.

The certification basis for parts changed or affected by the change since the reference date of application, August 24, 2015, is based upon part 27 as amended by Amendment 27-47. Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the latest amendment 27-0 through 27-47

27.29, 27.251, 27.301, 27.303, 27.305, 27.307, 27.337, 27.571, 27.601, 27.603, 27.605,

27.607, 27.609, 27.610, 27.613, 27.619, 27.771, 27.773, 27.777, 27.1301, 27.1307, 27.1321,

27.1322, 27.1351, 27.1357, 27.1367, 27.1381, 27.1525, 27.1529, 27.1541, 27.1555, 27.1581,

27.1583, 27.1585, 27.1589 Regulations at an intermediate amendment None.

Regulations at the amendment level in TCDS H88EU

27.561, 27.625, 27.853, 27.1309, 27.1365 ------------------------------------------------------------END-------------------------------------------------------